Full-Scale Firing Tests of Variable Flow Ducted Rocket Engines Employing Gap Solid Fuel Gas Generator

Author:

Nakayama Hisahiro,Ikegami Yoshiyuki,Yoshida Akihiko,Koori Kenji,Watanabe Kiyoyuki,Tokunaga Hidenori,Shimizu Haruo,Kanaizumi Shigeyuki

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Performance Analysis of a Ducted Rocket Under Various Flight Conditions;International Journal of Aeronautical and Space Sciences;2024-07-10

2. Study on Combustion Flow-Field of Solid Ducted Rocket with Multiple Gas Nozzles;2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE);2021-07-16

3. An LES for the Effects of Particle Size and Velocity Ratio on the Flow Structure in the Secondary Combustor;International Journal of Aeronautical and Space Sciences;2020-07-20

4. Experimental investigation of the effect of the air inlet angle and the combustion pressure in a ducted rocket combustor;Progress in Propulsion Physics – Volume 11;2019

5. A review of design issues specific to hypersonic flight vehicles;Progress in Aerospace Sciences;2016-07

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